X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Sun, 27 Jan 2013 20:47:53 -0500 Message-ID: X-Original-Return-Path: Received: from elasmtp-junco.atl.sa.earthlink.net ([209.86.89.63] verified) by logan.com (CommuniGate Pro SMTP 6.0.1) with ESMTP id 6032133 for lml@lancaironline.net; Sun, 27 Jan 2013 20:02:29 -0500 Received-SPF: none receiver=logan.com; client-ip=209.86.89.63; envelope-from=colyncase@earthlink.net DomainKey-Signature: a=rsa-sha1; q=dns; c=nofws; s=dk20050327; d=earthlink.net; b=Mz4wNc4qmsRZv6cObqI6OOb/3bZE8uGoHQSUaA72mjGItNTDDEyJCTLo6GQcFfwc; h=Received:Content-Type:Mime-Version:Subject:From:In-Reply-To:Date:Content-Transfer-Encoding:Message-Id:References:To:X-Mailer:X-ELNK-Trace:X-Originating-IP; Received: from [70.20.32.152] (helo=[192.168.1.24]) by elasmtp-junco.atl.sa.earthlink.net with esmtpa (Exim 4.67) (envelope-from ) id 1Tzd6i-0007AJ-7F for lml@lancaironline.net; Sun, 27 Jan 2013 20:01:56 -0500 Content-Type: text/plain; charset=us-ascii Mime-Version: 1.0 (Apple Message framework v1085) Subject: Re: [LML] Also, does the Primer work? From: Colyn Case In-Reply-To: X-Original-Date: Sun, 27 Jan 2013 19:01:55 -0600 Content-Transfer-Encoding: quoted-printable X-Original-Message-Id: References: X-Original-To: "Lancair Mailing List" X-Mailer: Apple Mail (2.1085) X-ELNK-Trace: 63d5d3452847f8b1d6dd28457998182d7e972de0d01da940736a11c437432109af66e06b2b91de21350badd9bab72f9c350badd9bab72f9c350badd9bab72f9c X-Originating-IP: 70.20.32.152 George, I don't have the whole answer but maybe one of the engine = experts will chime in. I do know: - engine pump does have a spring loaded bypass so that the boost pump = can drive fuel through it if it fails. (We learned that at the = Continental Factory course this week). - High boost is a speed function on the boost pump. I have never seen a = IV that didn't have one. - I'm not sure what the primer button does (I have both) but I think it = has special plumbing. Many planes don't have this. - I need to do some research to understand the relative outputs of the = engine pump vs. the boost pump and how that will affect mixture in the = event of an engine pump failure. My expectation is low boost will not = be enough and high boost will probably require a mixture adjustment. On Jan 27, 2013, at 12:30 PM, George Wehrung wrote: As a continuation to my previous post, referencing the build manual = chapters 14 and 23: Chapter 23: wiring: denotes a Single Pole Double Throw rocker switch = for the LOW-OFF-HIGH positions of the fuel boost pump. Chapter 14: Firewall Forward, depicting the fuel flow does not show a = separate routing for the fuel primer circuit. So how does the primer = function work? Is it merely pushing a higher volume of fuel through the = circuit? I know it's necessary for hot starts to quickly circulate the = cooler fuel to the manifold but does it somehow bypass the gascolator = and the engine driven fuel pump? This would make sense if it did as = some aircraft call for pushing in the primer and possibly holding it in = to keep the engine running in the event of an engine driven fuel pump = failure. So then why do I only have a low selection of the boost pump? Should I = replace my boost pump switch with a three-position LOW-OFF-HIGH switch. = Should I have the boost pump on LOW for takeoff, descent and landing? Thanks again George -- For archives and unsub = http://mail.lancaironline.net:81/lists/lml/List.html